US 4,248,534 AGranted

Apparatus and method for the elimination of angular vibration induced errors in ring laser gyroscopes

AssigneeThe Singer Company

InventorHubert F. Elbert

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Abstract

In a ring laser gyroscope which has a triangular block configuration, and which incorporates a triangular shaped laser resonant cavity defined by three corner mirrors, including an output mirror, the gyroscope is sinusoidally dithered to reduce lock-in effects at low angular rotational rates and the gyroscope output is corrected for error caused by lock-in at the extremities of each oscillation when the dither velocity is equal to zero by accumulating the ac voltage outputs of a photodiode measuring the light intensity of the interference pattern at each zero dither velocity and when the accumulated phase error reaches 2.pi. an overflow or borrow pulse is generated and added to the normal gyroscope output thereby correcting for the accumulated errors caused by lock-in at zero dither velocity.

Claims4

Dependent claims

In a sinusoidally dithered ring laser gyroscope wherein clockwise and counterclockwise light beams are generated in the optical cavity of the gyroscope and wherein the frequency differential between the two beams caused by rotation of the gyroscope results in an interference pattern when the beams are extracted from the gyroscope and heterodyned by a beam combining means and wherein the beat frequency of the interference pattern is measured by a photodetector and wherein the beat frequency is a measure of the angular rotation of the gyroscope and wherein means including the photodetector convert the measure of beat frequency to a gyroscope output signal indicating the angular rotation of the gyroscope, an apparatus comprising:

(a) said photodetector including at least one analog gyroscope output signal in the form
V(t) =Vp sin (.PSI.+.beta.+.phi.)
where Vp is a scale factor related to the excitation voltage of the photodetector means, .PSI. is the momentary phase difference between the clockwise and counterclockwise beams, .beta. is the composite scattering angle and .phi. is the fringe pattern adjustment for any phase which can be adjusted by positioning of the photodetector means;
(b) the excitation voltage of the photodetector being scaled such that ##EQU5## where .OMEGA..sub.L is the rate at which lock-in effect occurs in the gyroscope .OMEGA..sub.D is the dither rate of the gyroscope and .omega..sub.d is the dither frequency of the gyroscope;
(c) the fringe pattern adjustment .phi. being set at -.pi./4;
(d) means to sense said analog gyroscope output signal when the dither velocity is zero to obtain an error signal proportional to the phase error due to the lock-in phenomenon at said time;
and
(e) means to add said error signal to the gyroscope output signal to correct for phase errors due to the lock-in phenomenon.

5 more elements

Dependencies are inferred from the claim text.